Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:airfoil_series
|
| gptkbp:application |
high-speed aircraft
low-drag wings |
| gptkbp:characterizedBy |
laminar flow
improved drag characteristics |
| gptkbp:developedBy |
gptkb:National_Advisory_Committee_for_Aeronautics
|
| gptkbp:introducedIn |
1930s
|
| gptkbp:namingConvention |
6-series code (e.g., NACA 6412)
|
| gptkbp:notableFeature |
pressure recovery region
|
| gptkbp:optimizedFor |
laminar flow over a portion of the chord
specific lift coefficient |
| gptkbp:predecessor |
gptkb:NACA_4-series
gptkb:NACA_5-series |
| gptkbp:relatedTo |
gptkb:NACA_airfoil
|
| gptkbp:usedBy |
gptkb:aircraft
gptkb:Lockheed_P-80_Shooting_Star |
| gptkbp:usedIn |
gptkb:engineer
aeronautics |
| gptkbp:bfsParent |
gptkb:NACA_airfoil
gptkb:NACA_airfoil_series |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
NACA 6-series
|